Environmental Engineering Reference
In-Depth Information
TABLE 6.13
Mechanical.Properties.of.IM7/PPS.(Thermo-Lite TM. ) . Prepreg
LaminateProperty
FiberOrientation
TestData
K -1 Ratio
Fatigue.Strength,.Ksi
O 0
90 0
285
12.5
0.0117
0.083
Tensile.Modulus,.Msi
O 0
90 0
24,2
1.5
Compression.Strength,.Ksi
O 0
185
0.0108
2
T = Σ
Σ
ε
α
.
(6.33)
.
Table 6.14.gives.the.modulus.of.elasticity.and.coeficient.of.thermal.expan-
sion.for.the.prepreg.laminates.based.on.IM7.carbon.ibers.shown.in.Table 6.12.
and.Table 6.13. 26
The.10.percent.of.Boron.ibers.volume.fraction.added.to.IM7.iber..Strain.in.
different.layers.of.the.FRP.object.correlates.with.each.layer.
We. assume.that.correlation. between.strain.Δε 2 .during. delaminating. and.
number.of.cracks.are
.
Δε 2. =.(n*C) 1/2 .
(6.34)
Here:
n.is.a.number.of.cracks;
C.is.a.length.of.cracks.
Value.of.parameters.are.given.in.Table 6.15.
Figure 6.7.shows.the.measured.correlation.between.temperature.gradient.
and.strain.propagation.
Reference. 28. shows. the. test. stand. used. to. measure. delaminating. cracks..
Fiber.optic.sensors.are.embedded.in.the.FRP.package.and.they.detect.laser.
light.passing.through.the.material..The.infrared.camera.measures.tempera-
ture.at.the.side.surface.boundary.of.the.package..P.is.impulse.load,.M x .is.a.
bending.moment.
TABLE 6.14
Modulus.of.Elasticity.and.Coeficient.of.Thermal.Expansion.for.the.
Prepreg.Laminates
Material
IM7/PEEK
IM7/PPS
Modulus.of.Elasticity,.Msi
24.2
24.2
Coeficient.of.thermal.Expansion,.PPMF
-0.02
-0.06
 
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